Error Analysis of Total Lightning Location System Based on Monte Carlo Method

Author(s):  
Cai Li ◽  
Zou Xin ◽  
Wang Jianguo ◽  
Fan Yadong ◽  
Li Quanxin ◽  
...  
Atmosphere ◽  
2019 ◽  
Vol 10 (3) ◽  
pp. 149 ◽  
Author(s):  
Li Cai ◽  
Xin Zou ◽  
Jianguo Wang ◽  
Quanxin Li ◽  
Mi Zhou ◽  
...  

In the summer of 2013, a three-dimensional (3D)-based Foshan Total Lightning Location System (FTLLS), embedded with differential time of arrival (DTOA) techniques, was installed and started its operation in Foshan, Guangdong Province, China. In this paper, the geographical distribution and set-up information of FTLLS, the estimated locating errors and locating results, as well as its initial operation results are presented. FTLLS consists of nine sub-stations that receive electromagnetic waves associated with lightning discharges and locates VLF/LF (200 Hz–500 kHz) radiation sources in 3D. The remote sub-stations acquired triggered waveforms with a duration of 0.5 ms, a resolution of 12-bits, and a GPS-based sferic time tags of 24 h per day. Cloud-to-ground (CG) lightning events, intra-cloud (IC) lightning events and narrow bipolar events (NBEs) were located by FTLLS. Based on the Monte Carlo simulation, the two-dimensional horizontal location error is basically less than 100 m, and the vertical error (altitude) is less than 200 m when the lightning event occurs within the network. On the other hand, over 14 million lightning strikes were recorded successfully by FTLLS during the period of May to October in 2014, among which IC events, CG events and NBEs accounted for 65%, 34% and 1%, respectively. It is shown that FTLLS is capable of a fine three-dimensional (3D) location, in which the altitude parameters obtained are reasonable and well consistent with observed data in the previous studies. The location results of thunderstorms were additionally verified through simultaneously-observed radar data.


2021 ◽  
Vol 248 ◽  
pp. 105194
Author(s):  
Quanxin Li ◽  
Jianguo Wang ◽  
Li Cai ◽  
Mi Zhou ◽  
Yadong Fan

2013 ◽  
Vol 765-767 ◽  
pp. 1998-2003
Author(s):  
Yang Zhou ◽  
Ye Yan ◽  
Xu Huang ◽  
Teng Yi

The true trajectory of spacecraft disperses from the nominal due to kinds of errors and perturbations, including environment, actuator and sensor uncertainties. This paper studies the error analysis problem of closed-loop control for spacecraft orbital transfer via Monte Carlo method. At first, errors that affect the true state are introduced and a navigation-target-correction loop system for Monte Carlo simulation is built. A dynamical model for orbital transfer is established, based on which both the extended Kalman filter (EKF) algorithm and correction maneuver control algorithm are developed. Precision analysis is studied of high eccentric orbital (HEO) transfer under open-loop and closed-loop control respectively. The simulation results prove the validity of the proposed method.


2016 ◽  
Vol 372 ◽  
pp. 22-36 ◽  
Author(s):  
Sai Li ◽  
Yuan Yuan ◽  
Hao-Wei Zhang ◽  
Bin Liu ◽  
He-Ping Tan

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